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WO/2009/149904A2 |
An aircraft system carrier element (10) comprises a base body (12) made of a sound- and heat-insulating material, in which a climate channel (14), which is provided for supplying an aircraft compartment (22) and can be connected to an ai...
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WO/2009/150223A1 |
The present invention relates to a system for oxygen supply to persons in an aircraft. In order to provide as simple a system as possible that is suitable in particular for a reconfiguration of the seat devices (12), the system comprises...
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WO/2009/147161A1 |
The present invention provides an air inlet valve (2) for an airplane and a manufacturing method for an air inlet valve. The air inlet valve has an opening area (6) for ambient air (3) to pass therethrough to a internal fuselage area (7)...
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WO/2009/146843A1 |
The invention relates to a cooling system (10) for cooling a device (14) subjected to heat in a vehicle, particularly an aircraft, comprising a cooling circuit (12) permeated by a heat-carrying fluid and thermally coupled to the device (...
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WO/2009/144234A1 |
The invention relates to a fresh air inlet for an aircraft, comprising at least one ram air inlet (20) with at least one ram air inlet opening (36), at least one additional air inlet opening (26), situated at a distance from the ram air ...
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WO/2009/144162A1 |
A device for cooling exhaust air of aircraft air-conditioning systems (10), with a bypass duct (20) which bypasses an aircraft air-conditioning system, which is arranged downstream of a ram air duct (30) with a ram air inlet duct section...
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WO/2009/143954A1 |
A system (10) for ventilating an aircraft area (32, 34) comprises a ram-air duct (12) with an air inlet (14), a first ram-air duct branch (16) and a second ram-air duct branch (18) through which the flow can pass parallel to the first ra...
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WO/2009/141400A2 |
The invention relates to an inerting system for an aircraft, comprising at least one air separation module provided with at least one air inlet, a first air outlet and a second air outlet. Said air separation module is designed in such a...
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WO/2009/133218A1 |
The invention relates to a system comprising two independent pneumatic compressors (CAC) (2) with an electric power supply, connected to an independent CAC controller (5), and an auxiliary power unit (APU) (3) with dimensions such as to ...
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WO/2009/127652A2 |
The invention relates to a de-icing system for an aircraft, comprising at least one heat source (28) and at least one air discharging means (23) for discharging air in areas of the aircraft to be de-iced. The invention is characterized i...
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WO/2009/121557A1 |
The invention relates to a climate tube (10), particularly for airplanes, having an inner layer (12) and an outer layer (16) made of a fiber composite plastic material. In order to achieve high stiffness, while simultaneously maintaining...
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WO/2009/117408A1 |
A layered heater system is provided that includes an engineered substrate having an upper face sheet, a lower face sheet, and a core disposed between the upper face sheet and the lower face sheet. A dielectric layer is formed on at least...
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WO/2009/111677A2 |
Air treatment systems including an environmental control system, a mixer, an air distribution duct system, and one or more catalysts for treating the air in the aircraft cabin environment are provided. Methods for treating aircraft cabin...
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WO/2009/111776A1 |
A system for monitoring pressure change within at least one compartment of an aircraft is provided. The system includes a primary pressure sensor for providing a signal corresponding to a pressure within a primary compartment of the airc...
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WO/2009/106936A2 |
A device for delivering a breathing gas to an on-demand breathing mask (23) comprises - an Onboard Oxygen Generator (1 ) comprising an oxygen-rich gas outlet end; - compressor means (7) comprising inlet means (6) and outlet means (12), s...
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WO/2009/102524A1 |
A class divider for an aircraft passenger cabin is provided. The class divider includes a partition positioned immediately aft of a rear row of seats in a first predetermined class area of the aircraft cabin and an aft-facing panel havin...
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WO/2009/100897A1 |
The invention relates to a system (10) for ventilating an explosive region (12) of an aircraft, comprising a ram air channel (16), which has an air inlet for supplying ambient air into the ram air channel (16), and an air outlet (18). Th...
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WO/2009/093916A2 |
The subject of the invention is a group of new derivatives of aminoalkaπols, more specifically [(phenoxy)alkyl]aminoalkanols and [(phenoxy)acyl)aminoalkanols, their method of obtaining and their use for production of a medicine which is...
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WO/2009/090026A1 |
An air-conditioning system for an aircraft for the individual temperature control of regions (28, 30, 32, 34) of a cabin (28) of an aircraft, comprises a central air-conditioning device (2), which provides a pressurised and temperature-c...
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WO/2009/083558A2 |
The invention relates to a system for the prevention of icing in a conduit, as can occur in, for example, a conduit of an aircraft air conditioner. The system according to the invention has at least one sensor (10) for detecting mechanic...
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WO/2009/080168A1 |
The invention relates to an aircraft cooling system (10) comprising a cooling element (12) that comprises a housing (14), a cooling air inlet (18) that is embodied in the housing (14) and a plurality of heat exchangers (32, 34, 36, 38) t...
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WO/2009/073034A1 |
A comfort HVAC or refrigeration system includes a remote sensor for sensing an environmental condition within a climate-controlled space and having, an associated transmitter for sending, a wireless signal to a receiver of a controller s...
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WO/2009/068265A1 |
The invention relates to an energy supply system for operating at least one air conditioning system (26) of an aircraft, with at least one air line network and at least one electric line network, wherein the air line network is connected...
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WO/2009/064288A1 |
Aircraft environmental control systems having a single ram air inlet (201) providing air to both cabin compressors (204a, 204b) and associated heat exchangers are disclosed herein. In one embodiment, and environmental control system for ...
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WO/2009/053002A2 |
The invention relates to a system for air conditioning at least one partial region of an airplane, comprising an air supply device (18) for providing a region of the airplane that is to be ventilated with a desired temperature and with a...
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WO/2009/050006A2 |
The invention relates to a system for providing emergency oxygen and therapeutic oxygen in an aircraft, said system having an oxygen source (10), an oxygen conduction system (20) comprising a second oxygen outlet (21), a device for provi...
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WO/2009/042322A1 |
One embodiment of a pressure management system for an aircraft may include a cavity (24), an opening (46) in a surface of the cavity, and a moveable door (42). An interior area within the cavity may have an interior pressure and an exter...
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WO/2009/040389A1 |
The invention relates to an outlet valve (10) for an airplane, having a frame (12) for arranging in an opening (14) of an outer skin (16) of the airplane, a first cover (18) pivotally disposed in the frame (12) for controlling a flow cro...
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WO/2009/032497A1 |
Aircraft cabin airflow nozzles and associated systems and methods are disclosed. A system in accordance with a particular embodiment includes a cabin air nozzle (220) that in turn has a first passageway (223a) bounded at least in part by...
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WO/2009/019264A2 |
The invention relates to a valve for controlling a fluid flow from a first environment to a second environment, having a frame for disposing a separating element in the region of an opening, said element separating the first environment ...
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WO/2009/007094A2 |
The present invention relates to an air conditioning system (10) for an aircraft cabin (12) with at least one air inlet (14) for supplying air to the cabin (12), at least one air outlet (16) for discharging air from the cabin (12) and at...
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WO/2008/148973A2 |
The subject of the invention is an air outlet device fitted with a grid (10) fitted to an aerodynamic surface of an aircraft, wherein said grid comprises a plurality of openings defined by intermediate zones extending away from the aerod...
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WO/2008/143696A2 |
Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems are described herein. In one embodiment, a ram air inlet (201) configured in accordance with the present invention includes an...
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WO2008116628B1 |
A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and w...
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WO/2008/138846A2 |
A method and an apparatus for initiating a run-up procedure for a jet engine to avoid engine icing, the method comprising the following steps of providing at least one surface element that is made of a material suitable for ice in atmosp...
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WO/2008/138930A2 |
According to an exemplary embodiment of the invention an oxygen supply system for an aircraft is provided, wherein the said system comprises a control valve (5), a reservoir bag (3), a respiration device (1) and a sensor device (22), whe...
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WO/2008/140972A1 |
A cooling system for removing heat generated by electrical components (28) onboard aerospace vehicles flows coolant between an evaporator that removes heat from the component, and a condenser (52) within the skin (22,24) of the vehicle. ...
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WO/2008/135449A1 |
The invention relates to an aircraft including a cabin, in which the first parts of multiple multi-system connection devices are secured to at least one wall of the cabin. Each of said devices includes a male part or plug (80) and a fema...
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WO/2008/116862A1 |
A supply channel (1) with an air distribution system for vehicles, in particular for aircraft, is presented. The supply channel comprises an elongated housing (3), a hollow profile (5) extending in longitudinal direction of the housing, ...
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WO/2008/118973A2 |
A method for manufacturing a wall of a thin- walled structure is described. The method includes receiving parameters for the wall and one or more stiffening features associated with the wall via a user interface, providing the parameters...
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WO/2008/115273A2 |
A tandem inlet apparatus (10) for use with a high speed mobile platform, for example a commercial or military aircraft. The tandem inlet apparatus includes a Pitot inlet (102) for feeding air to a cabin air compressor (CAC) of an air con...
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WO/2008/112029A1 |
There is provided systems and methods for transporting heat away from galley refrigeration equipment (10) or other heat-generating systems such as avionics, power electronics, or in-flight entertainment units, via a potable water system ...
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WO/2008/101986A1 |
The present invention relates to a fuselage (1) of an aircraft or spacecraft, with at least one shell element (2) and a structural element (7). An interspace (5; 9) to which air can be admitted by an air stream (10) is provided between t...
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WO2008071319B1 |
An aircraft cooling system (1) according to the invention comprises a first coolant stream (4a) which cools at least one first heat load (2a), and a second coolant stream (4b) which cools at least one second heat load (2b), wherein the a...
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WO2008008324A9 |
There is provided systems and methods for transporting heat away from galley refrigeration equipment (12) or other heat-generating systems such as avionics, power electronics, or in-flight entertainment units, via a potable water system ...
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WO/2008/074433A1 |
The invention concerns a cooling system for an aircraft with an air inlet (4) through which air from the environment of the aircraft enters a ram air channel (2), and an air outlet (6) through which air emerges from the ram air channel (...
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WO/2008/065709A1 |
In supplying conditioned air in an airplane, conditioned air in which at least one of oxygen concentration and humidity has been regulated is produced in the airplane. The produced conditioned air is blown out through a plurality of air ...
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WO2007147259A9 |
Devices and systems are provided, that entrain ambient air within a primary stream of pressurised air, for use in a variety of applications including aircraft, buildings and other stationary structures. The ambient air is drawn through a...
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WO/2008/061712A1 |
The invention discloses the multistage cooling of an aircraft electronic system (2) with at least one electronic component which delivers heat. The multistage feature results from the use of a plurality of circuits for transferring the w...
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WO/2008/061713A1 |
A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) wh...
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